WO2006040140A1 - Kraftunterstützungsvorrichtung mit lastabhängiger kraftunterstützung - Google Patents
Kraftunterstützungsvorrichtung mit lastabhängiger kraftunterstützung Download PDFInfo
- Publication number
- WO2006040140A1 WO2006040140A1 PCT/EP2005/010968 EP2005010968W WO2006040140A1 WO 2006040140 A1 WO2006040140 A1 WO 2006040140A1 EP 2005010968 W EP2005010968 W EP 2005010968W WO 2006040140 A1 WO2006040140 A1 WO 2006040140A1
- Authority
- WO
- WIPO (PCT)
- Prior art keywords
- load
- power assist
- assist device
- force
- rocker arm
- Prior art date
Links
- 230000001419 dependent effect Effects 0.000 title claims abstract description 9
- 210000000078 claw Anatomy 0.000 claims description 19
- 238000005303 weighing Methods 0.000 claims description 19
- 230000005540 biological transmission Effects 0.000 claims description 4
- 238000013016 damping Methods 0.000 claims description 4
- 238000009434 installation Methods 0.000 description 3
- 238000001514 detection method Methods 0.000 description 2
- 230000000694 effects Effects 0.000 description 2
- 241001295925 Gegenes Species 0.000 description 1
- 238000010009 beating Methods 0.000 description 1
- 230000000903 blocking effect Effects 0.000 description 1
- 230000006835 compression Effects 0.000 description 1
- 238000007906 compression Methods 0.000 description 1
- 230000007547 defect Effects 0.000 description 1
- 210000003608 fece Anatomy 0.000 description 1
- 239000002655 kraft paper Substances 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 230000010355 oscillation Effects 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D11/00—Passenger or crew accommodation; Flight-deck installations not otherwise provided for
- B64D11/003—Stowage devices for passengers' personal luggage
-
- E—FIXED CONSTRUCTIONS
- E05—LOCKS; KEYS; WINDOW OR DOOR FITTINGS; SAFES
- E05F—DEVICES FOR MOVING WINGS INTO OPEN OR CLOSED POSITION; CHECKS FOR WINGS; WING FITTINGS NOT OTHERWISE PROVIDED FOR, CONCERNED WITH THE FUNCTIONING OF THE WING
- E05F1/00—Closers or openers for wings, not otherwise provided for in this subclass
- E05F1/08—Closers or openers for wings, not otherwise provided for in this subclass spring-actuated, e.g. for horizontally sliding wings
- E05F1/10—Closers or openers for wings, not otherwise provided for in this subclass spring-actuated, e.g. for horizontally sliding wings for swinging wings, e.g. counterbalance
- E05F1/1091—Closers or openers for wings, not otherwise provided for in this subclass spring-actuated, e.g. for horizontally sliding wings for swinging wings, e.g. counterbalance with a gas spring
-
- E—FIXED CONSTRUCTIONS
- E05—LOCKS; KEYS; WINDOW OR DOOR FITTINGS; SAFES
- E05Y—INDEXING SCHEME ASSOCIATED WITH SUBCLASSES E05D AND E05F, RELATING TO CONSTRUCTION ELEMENTS, ELECTRIC CONTROL, POWER SUPPLY, POWER SIGNAL OR TRANSMISSION, USER INTERFACES, MOUNTING OR COUPLING, DETAILS, ACCESSORIES, AUXILIARY OPERATIONS NOT OTHERWISE PROVIDED FOR, APPLICATION THEREOF
- E05Y2201/00—Constructional elements; Accessories therefor
- E05Y2201/40—Motors; Magnets; Springs; Weights; Accessories therefor
- E05Y2201/404—Function thereof
- E05Y2201/416—Function thereof for counterbalancing
-
- E—FIXED CONSTRUCTIONS
- E05—LOCKS; KEYS; WINDOW OR DOOR FITTINGS; SAFES
- E05Y—INDEXING SCHEME ASSOCIATED WITH SUBCLASSES E05D AND E05F, RELATING TO CONSTRUCTION ELEMENTS, ELECTRIC CONTROL, POWER SUPPLY, POWER SIGNAL OR TRANSMISSION, USER INTERFACES, MOUNTING OR COUPLING, DETAILS, ACCESSORIES, AUXILIARY OPERATIONS NOT OTHERWISE PROVIDED FOR, APPLICATION THEREOF
- E05Y2201/00—Constructional elements; Accessories therefor
- E05Y2201/60—Suspension or transmission members; Accessories therefor
- E05Y2201/606—Accessories therefor
- E05Y2201/618—Transmission ratio variation
-
- E—FIXED CONSTRUCTIONS
- E05—LOCKS; KEYS; WINDOW OR DOOR FITTINGS; SAFES
- E05Y—INDEXING SCHEME ASSOCIATED WITH SUBCLASSES E05D AND E05F, RELATING TO CONSTRUCTION ELEMENTS, ELECTRIC CONTROL, POWER SUPPLY, POWER SIGNAL OR TRANSMISSION, USER INTERFACES, MOUNTING OR COUPLING, DETAILS, ACCESSORIES, AUXILIARY OPERATIONS NOT OTHERWISE PROVIDED FOR, APPLICATION THEREOF
- E05Y2400/00—Electronic control; Electrical power; Power supply; Power or signal transmission; User interfaces
- E05Y2400/10—Electronic control
- E05Y2400/44—Sensors not directly associated with the wing movement
-
- E—FIXED CONSTRUCTIONS
- E05—LOCKS; KEYS; WINDOW OR DOOR FITTINGS; SAFES
- E05Y—INDEXING SCHEME ASSOCIATED WITH SUBCLASSES E05D AND E05F, RELATING TO CONSTRUCTION ELEMENTS, ELECTRIC CONTROL, POWER SUPPLY, POWER SIGNAL OR TRANSMISSION, USER INTERFACES, MOUNTING OR COUPLING, DETAILS, ACCESSORIES, AUXILIARY OPERATIONS NOT OTHERWISE PROVIDED FOR, APPLICATION THEREOF
- E05Y2600/00—Mounting or coupling arrangements for elements provided for in this subclass
- E05Y2600/10—Adjustable
- E05Y2600/11—Adjustable by automatically acting means
-
- E—FIXED CONSTRUCTIONS
- E05—LOCKS; KEYS; WINDOW OR DOOR FITTINGS; SAFES
- E05Y—INDEXING SCHEME ASSOCIATED WITH SUBCLASSES E05D AND E05F, RELATING TO CONSTRUCTION ELEMENTS, ELECTRIC CONTROL, POWER SUPPLY, POWER SIGNAL OR TRANSMISSION, USER INTERFACES, MOUNTING OR COUPLING, DETAILS, ACCESSORIES, AUXILIARY OPERATIONS NOT OTHERWISE PROVIDED FOR, APPLICATION THEREOF
- E05Y2900/00—Application of doors, windows, wings or fittings thereof
- E05Y2900/50—Application of doors, windows, wings or fittings thereof for vehicles
- E05Y2900/502—Application of doors, windows, wings or fittings thereof for vehicles for aircraft or spacecraft
-
- E—FIXED CONSTRUCTIONS
- E05—LOCKS; KEYS; WINDOW OR DOOR FITTINGS; SAFES
- E05Y—INDEXING SCHEME ASSOCIATED WITH SUBCLASSES E05D AND E05F, RELATING TO CONSTRUCTION ELEMENTS, ELECTRIC CONTROL, POWER SUPPLY, POWER SIGNAL OR TRANSMISSION, USER INTERFACES, MOUNTING OR COUPLING, DETAILS, ACCESSORIES, AUXILIARY OPERATIONS NOT OTHERWISE PROVIDED FOR, APPLICATION THEREOF
- E05Y2900/00—Application of doors, windows, wings or fittings thereof
- E05Y2900/50—Application of doors, windows, wings or fittings thereof for vehicles
- E05Y2900/53—Type of wing
- E05Y2900/538—Interior lids
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/40—Weight reduction
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T74/00—Machine element or mechanism
- Y10T74/20—Control lever and linkage systems
- Y10T74/20006—Resilient connections
Definitions
- the invention relates to a force assist device for providing a 'load-dependent supporting force.
- the invention relates to such a power assistance device for use in conjunction with a drop-down overhead luggage compartment in a passenger aircraft.
- Lowerable overhead luggage compartments in aircraft are known.
- a lowerable overhead luggage compartment of a Passagierflugzeu ⁇ ges with guide systems in the form of four-bar linkages on each side wall of the luggage compartment and a gas spring for each guide system that provides an assisting force for pivoting the luggage compartment according to the weight of the luggage compartment.
- An adjusting device detects the weight of the luggage compartment during loading and acts on the force application point of the gas spring via an adjusting connection in order to achieve a setting corresponding to the respective loading weight of the luggage compartment.
- a lowerable overhead luggage compartment which also has on its two side walls each have a guide system with a zugeord ⁇ Neten gas spring.
- the gas spring is operatively connected to a support device which provides a support force adapted to the weight of the luggage compartment for pivoting the luggage compartment upwards.
- a blocking device allows a locking of the support device.
- DE 44 46 772 Cl finally describes a device for guiding a ab ⁇ lowerable overhead luggage compartment with two arranged on both sides of the side walls of the luggage compartment four-bar linkages and a spring system per Gelenkvier ⁇ corner to support the high pivoting movement of the luggage compartment.
- An arranged inside the luggage compartment scale plate acts on below the scale plate arranged pressure transducer, which in turn are connected via at least one Verstelltell with an adjusting cylinder, which acts on an adjusting device for Ver ⁇ push the force application point of the spring system to move it depending on the weight of the luggage compartment so that an opposing torque adapted to the load moment resulting from the weight of the luggage compartment is provided.
- the invention has for its object to provide an improved device, which is suitable inter alia, in conjunction with a lowerable Matter ⁇ head luggage compartment of an aircraft to provide a dependent on the loading condition of the luggage compartment support force.
- the force-assisting device enables a purely mechanical control of a power assistance without the need for electrical or electronic components or actuators. According to an alternative, however, in the adjustment device and the load determining device of the invention
- the force-assisting device according to the invention is compact, has a mechanical structure in its essential components and can therefore be reliably operated independently of the current, as well as being light, which predestines it particularly for use in aircraft.
- 25 support device is essentially determined by the pivoting range of its support arm and the pivoting range of the rocker arm. If the force-assisting device according to the invention is used, for example, together with a lowerable overhead luggage compartment in an aircraft, the pivoting range of the oscillating lever is approximately 45 degrees, according to one embodiment. It understands
- the power assist device according to the invention is connected to one end of her Supporting arm pivotally attached to any support structure, while the other end of the support arm serves for connection to the object to which the Un ⁇ support force is to be applied.
- the oscillating lever of the adjusting device is released by the locking device in order to pivot the oscillating lever in this state of the adjusting device and thus adapt to loads of different weights
- the oscillating lever in all positions of the object between the open position and up to and including the closed position, the oscillating lever is at the point of its pivoting range extending from the first end position to the second end position iert, which corresponds to the detected load, so that one of the respectively detected load adapted support force is applied.
- the pivot axis of the pivot arm attached to the support arm is aligned End of the gas spring with the pivot axis of the pivotally mounted on the bearing plate end of the rocker arm.
- the locking device has a locking claw attached to the free end of the oscillating lever, which interacts with a circular-segment-shaped toothing.
- the latching claw is rotatably mounted at the end of the rocking lever and resiliently in the direction of engagement with the nikseg- - A -
- the detent ' claw is connected to a shift lever according to one embodiment, which is in the second position of the support arm, preferably of the attached thereto actuating and centering pin, so " actuated that the detent claw out of engagement with the toothing
- the shift lever is pivotably mounted on the fixed end of the rocker arm and the pivoting movement of the shift lever is transmitted via a cable or a linkage to the latching claw
- the support arm has at least one previously mentioned actuation
- the gas spring generating the assisting force is provided with a cap which actuates the shift lever in the second position of the support arm
- Embodiments preferably connected via a circular segment-shaped bridge with the bearing plate and the bearing plate is pivotally mounted on the support structure for adjusting said operating position.
- the power assist device acts in a preferred embodiment on the rocker arm a biasing force, which is directed opposite to a force exerted by the adjusting device with an increase in load on the rocker arm and which is such that it is the rocker arm in the load-free state pushes into its first end position.
- the first Endstel ⁇ ment is the position occupied by the rocker arm when no load is detected by the cooperating with the Verstellein ⁇ direction load detection device.
- the second end position of the oscillating lever is then the position which the oscillating lever occupies when the maximum assisting force of the force-assisting device is to take effect. This occurs when the load determining device detects the presence of a correspondingly large load.
- the adjustment movement of the rocker arm is damped. This prevents an uncontrolled oscillation of the oscillating lever after its unlocking and during an adjustment process.
- the biasing force acting on the rocker arm is generated by a damper gas spring unit, which at the same time causes the previously mentioned damping of rocker arm movement. Such an " embodiment is compact, inexpensive and reliable.
- the biasing force acting on the rocking lever is generated by at least one tension spring, one end of which is fixed to the bearing plate and the other end to the rocker arm.
- the load detection device has a pivotable Wä ⁇ geplatte, which is intended to receive a load and transmits their executed depending on the size of the load pivoting movement by means of a transmission device on the rocker arm.
- This transmission device can spielvati be a rope or a linkage. In such an embodiment, therefore, a changed load size is passed through a corresponding pivoting movement of the weighing plate directly to the rocker arm, which then - with unlocked locking device - adjusted to one of the new load size corresponding position.
- the load-determining device likewise has a weighing plate which is intended to receive a load, but this weighing plate is mounted on a plurality of load sensors in contrast to the previously described embodiment is to determine the load size, and further wherein the determined load size is reported to a controller, which adjusts the rocker arm according to the determined load size between its ers ⁇ th end position and its second end position.
- this actuator comprises an electric motor, which can exert an adjusting movement on the oscillating lever via a self-locking spindle drive.
- the spindle drive is designed to be self-locking, the combination of detent pawl and toothing described in connection with the purely mechanical design of the power assist device can be dispensed with, the self-locking spindle drive then represents the locking device for the rocker arm.
- the Load average is mechanically decoupled from the adjustment, no damping of the adjustment of the rocker arm provided to become.
- the pivotable articulation of the weighing plate is eliminated, instead, the weighing plate is floating on the load sensors (for example, four Lastsen ⁇ sensors) stored. This is an advantage, for example, when the weighing plate is at the bottom of a container, such as a luggage compartment, because the risk of ' jamming the pivotally hinged weighing plate deleted.
- the present invention power assist device can be anywhere get there dung to the applicational where loads are mainly move by manual forces from one position to another position and a maximum prescribed or reasonable operating force should not be exceeded.
- two preferred embodiments of a Kraftunterstützungsvor ⁇ invention direction in conjunction with a lowerable overhead luggage compartment in a passenger cabin of an aircraft with reference to the accompanying schematic drawings.
- FIG. 1 shows a side view of a better clarity because of partially dismantled power assist device for a lowerable overhead luggage compartment in an aircraft
- FIG. 2 is a perspective view of essential parts of the power assist device of FIG. 1;
- FIG. 3 shows the power assist device of FIG. 1 with an empty luggage compartment in a fully lowered, i.e. open position
- Figure 4 shows the power assist device of Figure 1 with the empty luggage compartment of Figure 3 in non-lowered, i. closed position
- FIG. 5 shows the power assist device of FIG. 1 with a maximum loaded luggage compartment in fully lowered, i. open position
- FIG. 6 shows the force-assisting device from FIG. 1 with a maximum loaded luggage compartment in a non-lowered, i. closed position
- Figure 7 is a side view of a modified embodiment of a Kraft ⁇ support device for a lowerable overhead luggage compartment in an aircraft, wherein the luggage compartment is empty and is in fully ab ⁇ lowered, ie open position,
- FIG. 8 shows the power assist device from FIG. 7 with the empty luggage compartment * in the non-lowered, ie closed, position.
- Figure 9 the power assist device of Figure 7 having a maximum laden NEN luggage compartment in a completely lowered, ie the open position
- FIG. 10 shows the power assist device of FIG. 7 with a maximum loaded luggage compartment in a non-lowered, i. closed position.
- FIG. 1 shows a side view of a force support device, generally designated 10, for providing a load-dependent assisting force for an only partially shown, lowerable overhead luggage compartment 12 in an aircraft.
- Figure 2 shows essential parts of the power assist device 10 for better understanding in a three-dimensional representation.
- the power assist device 10 is attached to a support structure, which is formed here by a traverse 14 of an otherwise not shown fuselage.
- the attachment of the power assist device 10 to the crossbar 14 by means of a bolt 16 to which on the one hand two bearing plates 18a, 18b and on the other hand, the one end of a support arm 20 are hinged.
- the bolt 16 defines an axis P about which the bearing plates 18a, 18b and in particular the support arm 20 are pivotable.
- the support arm 20 formed here from two spaced-apart plates 19a, 19b has a boomerang-shaped appearance and is fastened with its other end to the rear side of the luggage compartment 12.
- a gas spring 22 which serves to provide the support force to be applied by the force support device 10, on a pivot axis F hinged pivotally.
- the other end of the gas spring 22 is pivotally connected to the one, hinged in Figure 1 the lower end of a rocker arm 24, the other, in Figure 1 upper end on a protruding from the bearing plate 18 and a pivot axis Si defining bearing pin 26 is rotatably mounted.
- the rocker arm 24 has a U-shaped cross section (see Fig. 2).
- the bearing plates 18a, 18b have the outer shape of a circular sector, at the radially outer edge of which a bridge 28 establishes a connection between the two bearing plates 18a, 18b of the same shape and size.
- the bearing plate 18a is arranged in register with the bearing plate 18b and therefore * not shown in Figure 1 in order to allow a better visibility of the individual components of the power assist device 10.
- the shown in Figure 1 back "bearing plate 18b together with the in Fig. 1, not shown front Lager ⁇ plate 18a and the bridge 28 a type of housing, in which the whole kinematics of the power assist device 10 is received.
- the oscillating lever 24 can see within the angular range defined by the circular sector shape of the bearing plates 18a, 18b, which is approximately 45 degrees, about the bearing pin 26 and thus about the pivot axis Si a first end position, in which the force-assisting device 10 exerts no or almost no support force, and ver ⁇ be pivoted to a second end position in which the force-assisting device 10 delivers its maximum Unter ⁇ supporting force.
- This second end position of the rocker arm 24 is shown in FIG.
- a lever arm L between the axis P and a festge ⁇ by the pivotal attachment of the lower end of the gas spring 22 set pivot axis S 2 is maximum, so that the force generated by the gas spring 22 has its greatest effect on the support arm 20.
- the first end position of Schwinghe ⁇ lever 24 is located in Fig. 1 at the opposite edge of the bearing plates 18a, 18b in the clockwise direction. In this first end position, the pivot points of the axes P and S 2 and the pivot point F of the upper end of the gas spring 22 are approximately in line, ie, the lever arm L is zero or nearly zero, so that in this first end position virtually no support torque of the Gasdruckfe ⁇ 22 is exerted on the support arm 20.
- an arresting device In order to fix the oscillating lever 24 at a plurality of points between its first end position and its second end position, an arresting device is provided.
- This locking device essentially consists of a circular segment-shaped toothing 30 arranged on the bridge 28 and a latching claw 32 rotatably mounted on the free end of the oscillating lever 24, which is biased into engagement with the serration 30 by means of a compression spring 34 supported on the oscillating lever 24.
- the locking claw 32 is rotatable about the axis S 2 .
- the number of intermediate positions in which the Rocking lever 24 can be fixed by means of the locking device can be adjusted by a suitable design of the toothing 30 with more or fewer teeth in a wide range according to the requirements or wishes to be met.
- the rocker arm 24 can be locked by means of the Arret istsein- direction in its two end positions.
- an adjustment of the rocker arm 24 should only be possible in the open position of the luggage compartment 12, that is to say in the second position of the support arm 20.
- the latching claw 32 is spring-biased for engagement with the toothing 30, ie the oscillating lever 24 is normally locked.
- the locking In order to allow in the open position of the luggage compartment 12 a Verstel ⁇ development of the rocker arm 24, the locking must be canceled.
- a right in Figure 1 end of the locking claw 32 is connected via a linkage 36 with the one end of a shift lever 38 which is pivotally mounted on the upper end of the rocking lever 24 in Figure 1 about an axis E.
- the one end to which the linkage 36 is fixed, opposite end of the shift lever 38 is arcuate and designed to cooperate with an actuating and centering pin 40 which is attached to the support arm 20 near the Anlenkungspunk- tes the gas spring 22.
- This actuation and centering bolt 40 which in the exemplary embodiment shown is in each case provided on the outer side of the plates 19a, 19b, ie on both outer sides of the support arm 20, rests in the second position of the support arm 20, ie in the open position of the luggage compartment 12, in a formed on each bearing plate 18 a, 18 b centering recess 42 and presses on the arcuate arm of the shift lever 38, whereby it is pivoted counterclockwise about the axis E.
- the locking of the oscillating lever 24 in the exemplary embodiment shown should only be released when the support arm 20 is actually in its second position, ie the luggage compartment 12 is thus completely open.
- the bearing plate 18 can be limited by means of an adjusting screw 44 rotated about the axis P. With open luggage compartment 12, the force-assisting device 10 can be adjusted in such a way that the actuating and centering bolt 40 is located exactly in the centering recess 42.
- the load-dependent adjustment of the force-assisting device 10 will be explained in more detail with additional reference to FIGS. 3 to 6.
- the assisting force provided by the force-assisting device 10 varies as a function of the position of the oscillating lever 24.
- an adjusting device for pivoting the oscillating lever 24, there is an adjusting device, generally designated 46, to which a damper-gas-spring unit 48 belongs one end with the rocking lever 24 and the other end is pivotally connected to the attached to the luggage compartment 12 end of the support arm 20.
- this gas spring unit 48 serves to exert a biasing force on the oscillating lever 24, which presses the oscillating lever 24 in the load-free state into its first end position, in which the supporting force provided by the force-assisting device 10 assumes its minimum value.
- the gas spring unit 48 serves to dampen any pivoting movement of the rocker arm 24 in order to avoid an undesired "beating" of the rocker arm 24.
- these two functions - providing a Vorspann ⁇ force on the rocker arm and damping the pivoting movement of the Schwing ⁇ lever - summarized in the damper gas spring unit 48, however, these functions can also be exercised in a structurally separate manner by separate components.
- the adjusting device 46 cooperates with a load determining device 50 to determine the extent of a necessary adjustment of the oscillating lever 24.
- a load determining device 50 Comprises the load determining means 50 a at the front edge of the floor of the luggage compartment 12 with lateral loading 'demarcations 56.
- Figures 3 to 6 show the luggage compartment 12 in geöffne ⁇ ter and closed position, once without load and once with maximum load.
- Figure 3 shows the luggage compartment 12 in open, i.e. fully lowered position.
- the support arm 20 is thus in its second position.
- the swing lever 24 is therefore in its first end position, in the present embodiment, no or at most a very small support force is provided.
- FIG. 4 shows the luggage compartment 12 from FIG. 3 in its closed position.
- the support arm 20 assumes its first position, while the position of the rocker arm 24 in the position - in this case the first end position - is locked, which had been adjusted in the luggage compartment 12 open according to Figure 3.
- Figure 5 shows the luggage compartment 12 again in its open position, ie the support arm 20 is again in its second position, but is now on the weighing plate 54, the maximum load (not shown).
- the weighing plate 54 is pivoted downwardly compared to the state shown in FIG. 3 and " this pivoting movement has moved the oscillating lever 24 into its second end position.
- FIGS. 3 to 6 illustrate the possible extreme situations. It is understood that the oscillating lever 24 can also assume any position between its two end positions as a function of the load located on the weighing plate 54.
- FIGS. 7 to 10 show a second embodiment of a force-assisting device 110 for providing a load-dependent assisting force for a lowerable overhead luggage compartment 112 for a plurality of loading conditions and positions of the luggage compartment 112.
- identical parts carry the corresponding reference numerals of the first exemplary embodiment, which are increased by 100, however.
- the basic structural design and its function correspond to the first exemplary embodiment, for which reason only the differences between the design and the function of the first exemplary embodiment will be explained below.
- the second embodiment 110 has a reduced installation height and a reduced weight.
- the pivot axis F is moved slightly downwards and the gas pressure spring 122 has been provided with a cap 123, while the attachment point of the shift lever 138 has been relocated to the right with respect to the Figu ⁇ ren.
- the cap 123 can operate the shift lever 138.
- the actuating and centering pin 40 of the first embodiment is therefore in the second embodiment to a pure centering pin 140, which has only the task in the fully lowered, ie open position of the luggage compartment 112 to bring the pivot axes F and Si to cover.
- This aligned arrangement of the two pivot axes F and Si is achieved when the present on both sides of the support arm 120 centering pins 140 are received in the Zentriermulden 142 of the bearing plates 118a, 118b.
- the end of the switching lever 138 coming into contact with the cap 123 is provided with a roller 139.
- a linkage 160 the movement of the weighing plate 154 on a reversing lever 162, which in turn is articulated via a Switzerlandgestfite 166 with an eye 164 on the rocking lever 124.
- a damper is not provided in the second embodiment, instead, the tooth shape of the toothing 130 and the locking claw 132 are designed so that a leich ⁇ tes and secure locking and unlocking of the rocker lever 124 takes place upon actuation of the shift lever 138.
- the second embodiment also has two support springs 170 configured as over-center springs, only one of which is shown in FIGS. 7 to 10.
- One end of these support springs 170 is pivotally mounted to the bearing plates 118a and 118b, respectively, while its opposite other end is hinged to the plates 119a and 119b of the support arm 120, respectively.
- the support springs 170 exert a force which, in particular, securely holds an empty luggage compartment 112 in the open position and prevents a swinging of the opened luggage compartment.
- the adjusting screw 144 which serves as in the first embodiment for adjusting the open position of the luggage compartment 112, can additionally be used in the second embodiment as a transport safety. For this purpose, it is screwed with the luggage compartment open 112 in a threaded bore 172 of an arm 174 which is attached to the luggage compartment 112.
- the unit of force-assisting device " 110 and luggage compartment 112 can be well transported, for example, from the luggage compartment manufacturer to the aircraft plant .
- Figure 7 shows the luggage compartment 112 unloaded in the open position, the rocking lever 124 is in its first end position, the latching claw 132 is like seen from the teeth 130 solved.
- FIG. 8 shows the empty luggage compartment 112 from FIG. 7 in its closed position.
- the latching claw 132 is engaged with the teeth 130 and locks the rocker arm 124 in its first end position.
- FIG. 9 shows a maximally loaded luggage compartment 112 in the open position.
- the latching claw 132 is lifted out of the toothing 130 and the oscillating lever 124 has been moved to its second end position.
- FIG. 10 shows the maximum loaded luggage compartment 112 in its closed position.
- the rocking lever 124 is locked by means of the latching claw 132 and the toothing 130 in its second end position.
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Fluid-Damping Devices (AREA)
- Closing And Opening Devices For Wings, And Checks For Wings (AREA)
- Transmission Devices (AREA)
- Fittings On The Vehicle Exterior For Carrying Loads, And Devices For Holding Or Mounting Articles (AREA)
- Electrotherapy Devices (AREA)
- Vehicle Body Suspensions (AREA)
- Pivots And Pivotal Connections (AREA)
- Springs (AREA)
Priority Applications (6)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
BRPI0516843-0A BRPI0516843A (pt) | 2004-10-12 | 2005-10-12 | dispositivo de sustentação de força |
EP05797473A EP1799510B1 (de) | 2004-10-12 | 2005-10-12 | Kraftunterstützungsvorrichtung mit lastabhängiger kraftunterstützung |
CA2579919A CA2579919C (en) | 2004-10-12 | 2005-10-12 | Force supporting device with a load-dependent force support |
DE502005002451T DE502005002451D1 (de) | 2004-10-12 | 2005-10-12 | Kraftunterstützungsvorrichtung mit lastabhängiger kraftunterstützung |
JP2007536079A JP4521444B2 (ja) | 2004-10-12 | 2005-10-12 | 荷重に応じた力を補助する補助力発生装置 |
US11/576,728 US7481397B2 (en) | 2004-10-12 | 2005-10-12 | Force supporting device with a load-dependent force support |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE102004049700A DE102004049700B4 (de) | 2004-10-12 | 2004-10-12 | Kraftunterstützungsvorrichtung mit lastabhängiger Kraftunterstützung |
DE102004049700.1 | 2004-10-12 |
Publications (1)
Publication Number | Publication Date |
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WO2006040140A1 true WO2006040140A1 (de) | 2006-04-20 |
Family
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Family Applications (1)
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PCT/EP2005/010968 WO2006040140A1 (de) | 2004-10-12 | 2005-10-12 | Kraftunterstützungsvorrichtung mit lastabhängiger kraftunterstützung |
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US (1) | US7481397B2 (pt) |
EP (1) | EP1799510B1 (pt) |
JP (1) | JP4521444B2 (pt) |
CN (1) | CN100460245C (pt) |
AT (1) | ATE382509T1 (pt) |
BR (1) | BRPI0516843A (pt) |
CA (1) | CA2579919C (pt) |
DE (2) | DE102004049700B4 (pt) |
RU (1) | RU2355589C2 (pt) |
WO (1) | WO2006040140A1 (pt) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US7795252B2 (en) | 2004-12-20 | 2010-09-14 | Pfizer Inc. | Rapamycin analogues and the uses thereof in the treatment of neurological, proliferative, and inflammatory disorders |
Families Citing this family (27)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE102006045189B4 (de) * | 2006-09-25 | 2008-11-27 | Airbus Deutschland Gmbh | Kraftunterstützungssystem |
DE102007003363B4 (de) | 2007-01-23 | 2012-09-06 | Stabilus Gmbh | Kraftunterstützungsvorrichtung |
JP2009263944A (ja) * | 2008-04-24 | 2009-11-12 | Nifco Inc | 回動機構 |
AT506979B1 (de) * | 2008-07-11 | 2010-09-15 | Htp Aircraft Gmbh | Gepäckablage für ein passagierflugzeug |
US8317277B2 (en) * | 2009-04-21 | 2012-11-27 | Accuride International, Inc. | Dampened assisted-motion systems and methods |
US20100264793A1 (en) * | 2009-04-21 | 2010-10-21 | Accuride International, Inc. | Assisted-motion systems and methods |
DE102009057014B4 (de) | 2009-12-04 | 2012-05-03 | Diehl Aircabin Gmbh | Vorrichtung zum Schließen einer absenkbaren Schütte eines Gepäckfachs |
US9114867B2 (en) * | 2009-12-23 | 2015-08-25 | Bae Systems Plc | Air vehicle mounted transmitting or receiving equipment |
US8943751B2 (en) * | 2010-04-20 | 2015-02-03 | Be Intellectual Property, Inc. | Lift assist mechanism |
WO2011139918A2 (en) * | 2010-05-03 | 2011-11-10 | Jonathan Roberts | System and method for an automatically adjusting force engine and assisted storage |
US8770515B1 (en) * | 2010-06-02 | 2014-07-08 | The Boeing Company | Movement assistance system for a storage bin |
DE102011108895A1 (de) * | 2011-07-29 | 2013-01-31 | Airbus Operations Gmbh | Tragende Struktur für bewegliches Staufach |
DE102011118553B4 (de) * | 2011-11-16 | 2019-07-11 | Diehl Aviation Laupheim Gmbh | Gepäckablagefach für ein Flugzeug und Flugzeug mit dem Gepäckablagefach |
US8955805B2 (en) * | 2012-02-14 | 2015-02-17 | C&D Zodiac, Inc. | Pivot bin assembly |
DE102013003364B4 (de) * | 2013-03-01 | 2019-01-31 | General Aerospace GmbH | Kraftunterstützungsvorrichtung |
US20140260735A1 (en) * | 2013-03-15 | 2014-09-18 | Jonathan Roberts | Counterbalance system for assisting a user |
US9980564B2 (en) * | 2013-03-15 | 2018-05-29 | Jonathan Roberts | System and method for assembling and using assisted storage |
US9296479B1 (en) * | 2014-09-11 | 2016-03-29 | The Boeing Company | Stowage bin with closing force assistance |
CA3001883C (en) | 2015-11-03 | 2019-05-21 | Facc Ag | Overhead luggage compartment for an aircraft |
WO2018136955A1 (en) * | 2017-01-23 | 2018-07-26 | C&D Zodiac, Inc. | Pivot bin with lift assist assembly and method of use thereof |
US10836492B2 (en) | 2017-03-30 | 2020-11-17 | Itt Manufacturing Enterprises Llc | Load adaptive lift assist for pivoting stowage bin |
DE102017006493B4 (de) | 2017-07-08 | 2023-10-05 | Diehl Aviation Laupheim Gmbh | Staufach für den Überkopfbereich einer Passagierkabine |
WO2019018300A1 (en) | 2017-07-17 | 2019-01-24 | Harper Engineering Company | INTEGRATED LUGGAGE COMPARTMENT |
DE102017131130B4 (de) * | 2017-12-22 | 2023-05-04 | Airbus Operations Gmbh | Befestigungssystem zum Befestigen einer Komponente an einer Rumpfstruktur |
CN109733613B (zh) * | 2018-12-17 | 2024-02-13 | 航宇救生装备有限公司 | 一种座椅的整体角度调节机构 |
CN109747830B (zh) * | 2018-12-27 | 2022-04-19 | 中国航空工业集团公司西安飞机设计研究所 | 一种单组轮连杆式无人机投放装置及投放方法 |
JP2020196328A (ja) * | 2019-05-31 | 2020-12-10 | デルタ工業株式会社 | リンク機構、乗物の上部収容棚構造及びシートサスペンション機構 |
Citations (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE4130644A1 (de) * | 1991-09-14 | 1993-03-18 | Airbus Gmbh | Ueberkopf-gepaeckablage mit einer absenkbaren schale, insbesondere fuer ein passagierflugzeug |
Family Cites Families (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE4335151C2 (de) * | 1993-10-15 | 1996-09-26 | Daimler Benz Aerospace Airbus | Überkopf-Gepäckablage, insbesondere für ein Passagierflugzeug |
DE4446772C1 (de) * | 1994-12-24 | 1996-05-15 | Daimler Benz Aerospace Airbus | Vorrichtung zum Führen einer absenkbaren Schale für eine Überkopf-Gepäckablage, insbesondere in einem Passagierflugzeug |
AT402389B (de) * | 1995-10-04 | 1997-04-25 | Fischer Adv Components Gmbh | Sicherheitsvorrichtung für im flugzeuginnenraum angebrachte behälter sowie behälter für die luftfahrtindustrie |
DE19617657C2 (de) * | 1996-05-03 | 2001-04-26 | Eads Airbus Gmbh | Vorrichtung zum Führen einer absenkbaren Schale für eine Überkopf-Gepäckablage, insbesondere in einem Passagierflugzeug |
CA2242127C (en) * | 1997-07-07 | 2007-04-10 | Fischer Advanced Composite Components Gesellschaft M.B.H. | Container having a door |
US6045204A (en) * | 1998-10-13 | 2000-04-04 | Hexcel Corporation | Overhead stowage bins in aircraft |
DE19917657A1 (de) * | 1999-04-19 | 2000-11-09 | Odeko Verpackungsmaterialien G | Anlage und Verfahren zum Befüllen von Produktaufnahmen mit Produkten |
EP1260434B1 (en) * | 2001-05-24 | 2004-07-14 | Heath Tecna Inc. | Load assist mechanism for an overhead bin |
KR100428124B1 (ko) * | 2001-07-07 | 2004-04-28 | 현대자동차주식회사 | 차량 트렁크의 개폐시스템 및 그 설계방법 |
CN2501740Y (zh) * | 2001-09-11 | 2002-07-24 | 厦门金龙联合汽车工业有限公司 | 汽车内行李架 |
US6691951B2 (en) * | 2001-10-26 | 2004-02-17 | Britax Heath Tecna Inc. | Variable load assist mechanism for an overhead bin |
-
2004
- 2004-10-12 DE DE102004049700A patent/DE102004049700B4/de not_active Expired - Fee Related
-
2005
- 2005-10-12 AT AT05797473T patent/ATE382509T1/de not_active IP Right Cessation
- 2005-10-12 JP JP2007536079A patent/JP4521444B2/ja not_active Expired - Fee Related
- 2005-10-12 EP EP05797473A patent/EP1799510B1/de not_active Not-in-force
- 2005-10-12 US US11/576,728 patent/US7481397B2/en not_active Expired - Fee Related
- 2005-10-12 RU RU2007112674/11A patent/RU2355589C2/ru not_active IP Right Cessation
- 2005-10-12 CA CA2579919A patent/CA2579919C/en not_active Expired - Fee Related
- 2005-10-12 DE DE502005002451T patent/DE502005002451D1/de active Active
- 2005-10-12 BR BRPI0516843-0A patent/BRPI0516843A/pt not_active IP Right Cessation
- 2005-10-12 WO PCT/EP2005/010968 patent/WO2006040140A1/de active IP Right Grant
- 2005-10-12 CN CNB2005800345631A patent/CN100460245C/zh not_active Expired - Fee Related
Patent Citations (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE4130644A1 (de) * | 1991-09-14 | 1993-03-18 | Airbus Gmbh | Ueberkopf-gepaeckablage mit einer absenkbaren schale, insbesondere fuer ein passagierflugzeug |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US7795252B2 (en) | 2004-12-20 | 2010-09-14 | Pfizer Inc. | Rapamycin analogues and the uses thereof in the treatment of neurological, proliferative, and inflammatory disorders |
Also Published As
Publication number | Publication date |
---|---|
CN100460245C (zh) | 2009-02-11 |
CN101039821A (zh) | 2007-09-19 |
JP2008515721A (ja) | 2008-05-15 |
DE102004049700A1 (de) | 2006-04-13 |
RU2355589C2 (ru) | 2009-05-20 |
EP1799510B1 (de) | 2008-01-02 |
US20080035794A1 (en) | 2008-02-14 |
CA2579919A1 (en) | 2006-04-20 |
DE502005002451D1 (de) | 2008-02-14 |
DE102004049700B4 (de) | 2007-10-18 |
JP4521444B2 (ja) | 2010-08-11 |
EP1799510A1 (de) | 2007-06-27 |
BRPI0516843A (pt) | 2008-09-23 |
CA2579919C (en) | 2010-09-21 |
ATE382509T1 (de) | 2008-01-15 |
RU2007112674A (ru) | 2008-11-27 |
US7481397B2 (en) | 2009-01-27 |
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